The Space Power Satellite(SPS) would be a huge spacecraft capturing the power of solar radiation in space and to supply electric power to the electric grid on the ground. The SPS concept was proposed by Dr. Peter Glas...The Space Power Satellite(SPS) would be a huge spacecraft capturing the power of solar radiation in space and to supply electric power to the electric grid on the ground. The SPS concept was proposed by Dr. Peter Glaser in 1968. SPS have been studied now for exactly fifty years by many scientists in various countries. It has been regarded as one of the most promising energy projects of the future and has been attracting more attention in recent years. More and more Chinese scholars and experts are paying attention to the development of SPS. Due to the huge size, immense mass and high power of such a satellite system, there are many technical difficulties which exist to realize SPS. In this paper, recent SPS research and development activities are reviewed first. Various SPS concepts are analyzed and compared. The primary scheme of the Multi-Rotary joint SPS(MR-SPS) is described. The main feature is that the huge solar array comprising many separate small solar sub-arrays and each solar sub-array has two middle power rotary joints. So, the most challenging technology, the high-power rotary joint, is simplified by using many middlepower rotary joints hence the possibility of a single-point failure of a single rotary joint is avoided. This enables easy assembly of the modular solar arrays. Finally some key technologies of MR-SPS are analyzed.展开更多
As a result of Japan raising the alert level at its quake-damaged nuclear plant from four to seven on a seven-point international scale of atomic incidents,which was caused by the 9.0-magnitude earthquake
The concept of a space solar power station(SSPS)was proposed in 1968 as a potential approach for solving the energy crisis.In the past 50 years,several structural concepts have been proposed,but none have been sent in...The concept of a space solar power station(SSPS)was proposed in 1968 as a potential approach for solving the energy crisis.In the past 50 years,several structural concepts have been proposed,but none have been sent into orbit.One of the main challenges of the SSPS is dynamic behavior prediction,which can supply the necessary information for control strategy design.The ultra-large size of the SSPS causes difficulties in its dynamic analysis,such as the ultra-low vibration frequency and large fexibility.In this paper,four approaches for the numerical analysis of the dynamic problems associated with the SSPS are reviewed:the finite element,absolute nodal coordinate,foating frame formulation,and structure-preserving methods.Both the merits and shortcomings of the above four approaches are introduced when they are employed in dynamic problems associated with the SSPS.Synthesizing the merits of the aforementioned four approaches,we believe that embedding the structure-preserving method into finite element software may be an effective way to perform a numerical analysis of the dynamic problems associated with the SSPS.展开更多
现有关于空间太阳能电站(Space Solar Power Station,SSPS)轨道动力学的研究中,均将其放置于地球静止轨道(Geostationary Orbit,GEO),然而这并非最优的工作轨道。文章提出了一种优于GEO的地球同步拉普拉斯(Geosynchronous Laplace Plane...现有关于空间太阳能电站(Space Solar Power Station,SSPS)轨道动力学的研究中,均将其放置于地球静止轨道(Geostationary Orbit,GEO),然而这并非最优的工作轨道。文章提出了一种优于GEO的地球同步拉普拉斯(Geosynchronous Laplace Plane,GLP)轨道。首先,建立了轨道运动模型及影响轨道运动的摄动模型,包括地球非球形引力摄动、日月引力摄动、太阳光压力摄动及微波反冲力摄动;然后,提出了评估空间太阳能电站轨道的3个指标:接收功率、轨道适用性和安全性,并据此分析了GLP轨道相对于GEO的优势。最后,给出了数值仿真算例。结果表明:在发电功率大致相同且满足供电需求的情况下,工作在GLP上的SSPS每年大约能节省用于轨道保持的燃料36 453.4kg。展开更多
针对多旋转关节空间太阳能电站(Space Solar Power Station,SSPS),提出一种环形拓扑的电力系统架构。基于功率分层准则对SSPS电力拓扑架构进行设计,提出U1～U7共7个层级、母线电压5000V、功率等级为MW的太阳能电站电力系统。针对分层架...针对多旋转关节空间太阳能电站(Space Solar Power Station,SSPS),提出一种环形拓扑的电力系统架构。基于功率分层准则对SSPS电力拓扑架构进行设计,提出U1～U7共7个层级、母线电压5000V、功率等级为MW的太阳能电站电力系统。针对分层架构中多太阳电池阵子阵并联(U6层),提出分层功率平衡统一控制策略,对MPPT控制、MPPT控制+稳定直流母线电压混合控制、MPPT算法+下垂稳定直流母线电压混合控制三种控制方法开展仿真分析。结果表明,提出的基于虚拟阻抗的下垂控制策略可以有效调节、分配功率,解决了空间发电站母线电压无法稳定的问题。展开更多
文摘The Space Power Satellite(SPS) would be a huge spacecraft capturing the power of solar radiation in space and to supply electric power to the electric grid on the ground. The SPS concept was proposed by Dr. Peter Glaser in 1968. SPS have been studied now for exactly fifty years by many scientists in various countries. It has been regarded as one of the most promising energy projects of the future and has been attracting more attention in recent years. More and more Chinese scholars and experts are paying attention to the development of SPS. Due to the huge size, immense mass and high power of such a satellite system, there are many technical difficulties which exist to realize SPS. In this paper, recent SPS research and development activities are reviewed first. Various SPS concepts are analyzed and compared. The primary scheme of the Multi-Rotary joint SPS(MR-SPS) is described. The main feature is that the huge solar array comprising many separate small solar sub-arrays and each solar sub-array has two middle power rotary joints. So, the most challenging technology, the high-power rotary joint, is simplified by using many middlepower rotary joints hence the possibility of a single-point failure of a single rotary joint is avoided. This enables easy assembly of the modular solar arrays. Finally some key technologies of MR-SPS are analyzed.
文摘As a result of Japan raising the alert level at its quake-damaged nuclear plant from four to seven on a seven-point international scale of atomic incidents,which was caused by the 9.0-magnitude earthquake
基金supported by the National Natural Science Foundation of China(12172281,11972284,11672241,11432010,and 11872303)Fund for Distinguished Young Scholars of Shaanxi Province(2019JC-29)+2 种基金Foundation Strengthening Program Technical Area Fund(2021-JCJQ-JJ-0565)Fund of the Science and Technology Innovation Team of Shaanxi(2022TD-61)Fund of the Youth Innovation Team of Shaanxi Universities.
文摘The concept of a space solar power station(SSPS)was proposed in 1968 as a potential approach for solving the energy crisis.In the past 50 years,several structural concepts have been proposed,but none have been sent into orbit.One of the main challenges of the SSPS is dynamic behavior prediction,which can supply the necessary information for control strategy design.The ultra-large size of the SSPS causes difficulties in its dynamic analysis,such as the ultra-low vibration frequency and large fexibility.In this paper,four approaches for the numerical analysis of the dynamic problems associated with the SSPS are reviewed:the finite element,absolute nodal coordinate,foating frame formulation,and structure-preserving methods.Both the merits and shortcomings of the above four approaches are introduced when they are employed in dynamic problems associated with the SSPS.Synthesizing the merits of the aforementioned four approaches,we believe that embedding the structure-preserving method into finite element software may be an effective way to perform a numerical analysis of the dynamic problems associated with the SSPS.
文摘现有关于空间太阳能电站(Space Solar Power Station,SSPS)轨道动力学的研究中,均将其放置于地球静止轨道(Geostationary Orbit,GEO),然而这并非最优的工作轨道。文章提出了一种优于GEO的地球同步拉普拉斯(Geosynchronous Laplace Plane,GLP)轨道。首先,建立了轨道运动模型及影响轨道运动的摄动模型,包括地球非球形引力摄动、日月引力摄动、太阳光压力摄动及微波反冲力摄动;然后,提出了评估空间太阳能电站轨道的3个指标:接收功率、轨道适用性和安全性,并据此分析了GLP轨道相对于GEO的优势。最后,给出了数值仿真算例。结果表明:在发电功率大致相同且满足供电需求的情况下,工作在GLP上的SSPS每年大约能节省用于轨道保持的燃料36 453.4kg。
文摘针对多旋转关节空间太阳能电站(Space Solar Power Station,SSPS),提出一种环形拓扑的电力系统架构。基于功率分层准则对SSPS电力拓扑架构进行设计,提出U1～U7共7个层级、母线电压5000V、功率等级为MW的太阳能电站电力系统。针对分层架构中多太阳电池阵子阵并联(U6层),提出分层功率平衡统一控制策略,对MPPT控制、MPPT控制+稳定直流母线电压混合控制、MPPT算法+下垂稳定直流母线电压混合控制三种控制方法开展仿真分析。结果表明,提出的基于虚拟阻抗的下垂控制策略可以有效调节、分配功率,解决了空间发电站母线电压无法稳定的问题。
